公开(公告)号：US20140343907A1

公开(公告)日：2014-11-20

申请号：US14274984

申请日：2014-05-12

Applicant: Thales

Inventor： Pierre GAMET ,  Rémy AULETTO

IPC: G06F17/50

CPC classification number: G06F17/5009 ,  G08G5/065

Abstract: This building method concerns building of at least one aircraft guideline in an airport navigation network. The navigation network includes a plurality of polygons and is associated with an airport area including taxiways, each guideline connecting two distinct sides of a corresponding polygon, the navigation network being configured to be stored in a memory of a computer system. The method is implemented by a computer and includes the following steps creating nodes at each intersection between an existing guideline and a side of a corresponding polygon, or at the middle of a side shared by two polygons when no guideline is secant with said side, detecting at least one pair of nodes not connected by a guideline, computing, for each detected pair of nodes, a guideline in the form of a polynomial curve, and storing the computed guidelines in the memory of the computer system.

Abstract translation: 这种建筑方法涉及在机场导航网络中建立至少一个飞行器准则。 导航网络包括多个多边形，并且与包括滑行道的机场区域相关联，每个指南连接相应多边形的两个不同侧，导航网络被配置为存储在计算机系统的存储器中。 该方法由计算机实现，并且包括以下步骤：在现有的指南和对应的多边形的一侧之间的每个交叉点处创建节点，或者当没有准则与所述侧面正交时由两个多边形共享的一侧的中间 至少一对不由指南连接的节点，对于每个检测到的一对节点，计算多项式曲线形式的准则，并将计算出的准则存储在计算机系统的存储器中。

公开(公告)号：US20160210867A1

公开(公告)日：2016-07-21

申请号：US14992929

申请日：2016-01-11

Applicant: THALES

Inventor： Christophe PIERRE ,  Rémy AULETTO ,  Benoît DACRE-WRIGHT

IPC: G08G5/00 ,  G01W1/02 ,  G06F7/72 ,  G01C21/20

CPC classification number: G08G5/0039 ,  G01C21/20 ,  G01W1/02 ,  G06F7/724 ,  G08G5/0034 ,  G08G5/0052 ,  G08G5/0091

Abstract: A navigation aid method for an aircraft flying a reference trajectory between a point of departure and a point of arrival subject to a field of wind vectors comprises: decomposing the reference trajectory into a plurality of discrete waypoints Pi, loading meteorological data comprising the field of wind vectors, iterating the following steps N times, to generate an improved trajectory: for each waypoint Pi named current point, determining a reference plane, determining an orthonormal reference frame, determining a wind curl ((∇W)Pi), determining a sign of the projection of the wind curl on axis zi ((∇W)zi Pi), determining a direction of displacement from the current point Pi to a new current waypoint Pi′, determining a line of displacement, determining a displacement distance, determining the new current waypoint, determining a new trajectory, assigning the new waypoints Pi′ determined in the preceding iteration to the waypoints Pi for the next iteration.

Abstract translation: 一种用于飞行在出发点与受到风向量场的到达点之间的参考轨迹的飞行器的导航辅助方法包括：将参考轨迹分解为多个离散航路点Pi，加载包括风场的气象数据 向量，迭代以下步骤N次，以产生改进的轨迹：对于每个路点Pi命名当前点，确定参考平面，确定正交参考帧，确定风卷曲（（∇W）Pi），确定 确定从当前点Pi到新的当前路点Pi'的位移方向，确定位移线，确定位移距离，确定新的当前点Pi 确定一个新的轨迹，将上一次迭代中确定的新路点Pi'分配给下一次迭代的路点Pi。

公开(公告)号：US20160210866A1

公开(公告)日：2016-07-21

申请号：US14991704

申请日：2016-01-08

Applicant: THALES

Inventor： Christophe PIERRE ,  Rémy AULETTO ,  Benoît DACRE-WRIGHT

IPC: G08G5/00 ,  G01C21/00

Abstract: A navigational aid method of an aircraft, carried out by a flight management system, for comparing a reference trajectory of the aircraft subjected to a wind vector field with a new trajectory between the same starting and end points, respectively, the method comprises: determining the reference trajectory, determining the new trajectory, loading meteorological data, determining a directional surface, delimited by a directional closed curve, consisting of the new trajectory, from the starting point to the end point, closed by the opposite of the reference trajectory from the end point to the starting point, determining a wind curl on the basis of the wind vector field, determining a flow of the wind curl through the surface, a positive value of flow indicating that the new trajectory makes better use of the wind load, a negative value of flow indicating that the new trajectory makes less effective use of the wind load.

Abstract translation: 一种由飞行管理系统执行的用于将经过风矢量场的飞行器的参考轨迹与相同起点和终点之间的新轨迹进行比较的飞行器的导航辅助方法，包括：确定 参考轨迹，确定新的轨迹，加载气象数据，确定由方向性闭合曲线限定的方向表面，由新的轨迹组成，从起始点到终点，与从末端到参考轨迹的相反闭合 指出起点，根据风矢量场确定风卷曲，确定通过表面的卷曲流动，表示新轨迹更好地利用风荷载的流量正值，负值 流量值指示新的轨迹使得风力负荷的使用效果较差。

公开(公告)号：US20160085239A1

公开(公告)日：2016-03-24

申请号：US14861610

申请日：2015-09-22

Applicant: THALES

Inventor： Johan BOYER ,  Rémy AULETTO ,  Norbert BALOCHE

IPC: G05D1/04 ,  G05D1/06 ,  G01C21/00

CPC classification number: G05D1/042 ,  G01C21/00 ,  G01C23/00 ,  G05D1/0676 ,  G08G5/0021 ,  G08G5/025 ,  Y02T50/84

Abstract: A method for adapting an aircraft constant-gradient descent segment comprises: an acquisition step in which state variables characterizing the aircraft, environment variables characterizing the environment thereof and path variables characterizing the predicted path thereof at one of the initial and final points of the segment are acquired; a calculation step whereby a limit ground gradient for at least one performance criterion is calculated from the state variables, environment variables and path variables; a validity verification step checking the validity of the path initially predicted against the most restrictive limit ground gradient; and when the path initially predicted is not valid: a feasibility verification step checking the feasibility of a command to modify at least one state variable; if feasibility is verified, a prediction of executing the command; otherwise, a prediction of modifying one of the initial and final points of the segment with respect to constraints of the flight plan.

Abstract translation: 一种用于调整飞行器恒定梯度下降段的方法，包括：获取步骤，其中表征飞行器的状态变量，表征其环境的环境变量和表征其在该段的初始和最终点之一的预测路径的路径变量是 获得 计算步骤，其中根据状态变量，环境变量和路径变量计算至少一个性能标准的极限地面梯度; 有效性验证步骤，根据最严格限制的地面坡度检查最初预测的路径的有效性; 并且当最初预测的路径无效时：可行性验证步骤检查命令修改至少一个状态变量的可行性; 如果验证可行性，则执行命令的预测; 否则，预测相对于飞行计划的约束修改段的初始和最终点之一。